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Zenith STOL CH 750
6.4 PERMITTED PAYLOAD RANGE / CALCULATION SAMPLES
Max Gross Weight:
Max Forward CG:
Max Aft CG:
ITEM
A/C Empty Weight
Pilot
Passenger
Wing Tanks, Fuel *
Baggage
TOTALS
LOADED WEIGHT
ITEM
A/C Empty Weight
Pilot
Passenger
Wing Tanks, Fuel *
Baggage
TOTALS
LOADED WEIGHT
* MOGAS = 0.72 kg/ Liter
Issued: 01.02.2020
Airplane Flight Manual
= 600 kg
= 280 mm
= 500 mm
MOST ADVERSE FORWARD
Weight
Arm (mm)
(kg)
360
70
0
11
0
1600
451
^ ^ ^ ^ ^ ^
CG (mm)
MOST ADVERSE AFT
Weight
Arm (mm)
(kg)
360
77
77
68
18
1600
600
^ ^ ^ ^ ^ ^
CG (mm)
Revision 0, Dat. 01.02.2020
Moment Fuel (ltr)
361
129'960
545
38'150
545
0
630
69'30
0
203'840
452
Moment Fuel (ltr)
361
129'960
545
41'965
545
41'965
630
42'840
28'800
285'530
476
HB-YRC
15
90
Page 63-93
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